首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   142篇
  免费   37篇
  国内免费   44篇
航空   120篇
航天技术   31篇
综合类   18篇
航天   54篇
  2024年   1篇
  2023年   8篇
  2022年   14篇
  2021年   16篇
  2020年   6篇
  2019年   13篇
  2018年   10篇
  2017年   3篇
  2016年   1篇
  2015年   3篇
  2014年   4篇
  2013年   12篇
  2012年   9篇
  2011年   18篇
  2010年   10篇
  2009年   9篇
  2008年   4篇
  2007年   6篇
  2006年   9篇
  2005年   5篇
  2004年   4篇
  2003年   2篇
  2001年   1篇
  2000年   3篇
  1999年   9篇
  1998年   2篇
  1997年   3篇
  1996年   3篇
  1995年   5篇
  1994年   2篇
  1993年   7篇
  1992年   4篇
  1991年   4篇
  1990年   4篇
  1989年   6篇
  1988年   2篇
  1987年   1篇
排序方式: 共有223条查询结果,搜索用时 15 毫秒
131.
考虑时间约束的无人飞行器航迹规划   总被引:1,自引:0,他引:1  
在分析时间误差分配的基础上,本文提出了一种考虑时间约束的航迹规划方法.该方法对传统的航迹结构进行了改进,通过速度调整策略和在代价函数中加入时间约束驱使算法找到使到达目标点时间误差尽可能小的航迹.同时,分别研究了起飞时间误差,速度调节能力及飞行速度误差三个因素对到达目标点时间误差的不同影响.  相似文献   
132.
长椭圆球波函数在卫星导航中的应用研究   总被引:2,自引:0,他引:2  
卫星导航信号的码片波形是影响系统跟踪精度和抗多径干扰性能的重要因素。首次提出将时域上集中分布同时在频域上能量聚集性最佳的长椭球波函数(Prolate Spheroidal Wave Functions,PSWF)作为导航信号码片波形,并对比分析了相同码速率和带宽限制下的PSWF码片波形和二进制偏移载波(Binary Offset Carrier,BOC)调制码片波形的跟踪和抗多径性能。结果表明:在合适的带宽范围内,PSWF码片波形具有和带限BOC调制码片波形结构相似的相关函数和功率谱密度;PSWF码片波形在跟踪精度和抗多径干扰方面整体上优于带限BOC调制码片波形。综合分析,PSWF码片波形具备较好的导航性能,可作为我国卫星导航信号波形设计的一种新选择。  相似文献   
133.
超高强度钢立铣工件温度分析及对加工表面质量的影响   总被引:1,自引:0,他引:1  
杨升  董琼  彭芳瑜  林森  闫蓉 《航空学报》2015,36(5):1722-1732
以航空难加工材料300M钢为研究对象,基于立铣加工中的工件温度判断在铣削加工中是否出现了金相组织转变,进而分析不同工况下影响加工表面质量的因素。首先,将移动热源法应用于铣削加工中,计算考虑后刀面磨损的立铣加工工件温度,实验表明,计算值与实验值相比误差在10%以内。然后,分析了工件温度在时间上与空间上的分布,以及不同刀具磨损和加工参数条件下工件表面的温升规律,据此预测加工表面是否出现了组织转变,并结合金相组织观察进一步确认。最后,依据加工表面质量物理层面残余应力和显微硬度的检测数据,初步探讨了各因素对表面质量的影响。结果表明,在研究的加工参数范围内,并未达到金相组织转变温度,表面质量主要受铣削热力作用下的剪切面塑性凸出效应、后刀面挤光效应和热效应的影响。  相似文献   
134.
Man's quest to get into space is hindered by major problems (e.g., system-development and capital costs, expense of putting mass into orbit, trapped-radiation belts, and environmental impact of a large increase in rocket launches). A multi-purpose low-earth-orbit system of rings circling the earth – the “LEO ARCHIPELAGOTM” – is proposed as a means of solving or bypassing many of them. A fiber-optic ring about the earth would be an initial testing and developmental stage for the Ring Systems, while providing cash-flow through a LEO-based, high-band-width, world-wide communication system. A low-earth-orbit-based space-elevator system, “Sling-on-a-RingTM”, is proposed as the crucial developmental stage of the LEO Archipelago. Being a LEO-based heavy-mass lifter, rather than earth- or GEO-based, it is much less massive and therefore less costly than other proposed space-elevators. With the advent of lower-cost, higher-mass transport to orbit, the options for further space development (e.g., space solar power, radiation, and space-debris dampers, sun shades, and permanent LEO habitation) are greatly expanded.This paper provides an update of the Sling-on-a-Ring concept in terms of new materials, potential applications, and trade-offs associated with an earlier model. The impact of Colossal Carbon Tubes, CCT, a new material with high tensile strength, extremely-low density, and other favorable properties, and other new technologies (e.g., solar-powered lasers, power beaming to near-space and earth, and thermal-control systems) on the development of associated LEO-Ring systems is also explored. The material's effect on the timeline for the system development indicates the feasibility of near-term implementation of the system (possibly within the decade). The Sling-on-a-Ring can provide a less-expensive, environment-friendly mode of access to space. This would pave the way (via eventual operation at >1000 t per day by 2050) for large scale development of space-based technologies.  相似文献   
135.
阐述提高HTML语言与应用课程课堂教学质量的方法,并从实践的角度探讨这些方法的有效性。  相似文献   
136.
We investigate the north–south (N–S) asynchrony of the polar faculae and compare it with the hemispheric asynchrony of solar activity at low latitudes. We find that, (1) both the solar activity at high and low latitudes do not synchronously occur in the northern and southern hemispheres, there is phase shifts between the two hemispheres; (2) the N–S asynchrony of the polar faculae is a function of latitudes, implying that the asynchrony of the polar faculae between the two hemispheres is related to the hemispheric asymmetry and latitudinal distribution of the polar faculae.  相似文献   
137.
提出一套基于EC5—1612CVDNA的自动化输送系统网络数字化视频监控解决方案。  相似文献   
138.
Many review articles have been written on the topic of the aerodynamics of slender bodies at incidence, some of which are referenced in this paper. Here, we review the unsteady behavior of these flows. Our aim is to review the material that contributes to our understanding of unsteady phenomena over slender bodies at incidence. Natural unsteadiness is explored first. Unexpectedly, we found a large number of contributions in this area. We found the material disjointed, making it difficult to draw general conclusions. Forced unsteadiness is conceptually easier to follow, but the number of contributions on this topic is much smaller. We consider both experimental and numerical contributions but we do not discuss the corresponding methodologies.  相似文献   
139.
大气湍流通常会造成激光光斑畸变为不规则的异形光斑,针对目前四象限探测器(QD)对空间光通信中不规则光斑偏转角度测量精度不足的问题,提出了一种基于多源信息融合的高精度光束偏转角度测量方法.该方法通过对QD及电荷耦合元件(CCD)的数据信息进行融合分析,在保持QD高分辨率和高响应速度的基础上,提高QD对不规则光斑偏转角的测...  相似文献   
140.
To hit stationary ground targets in specified direction, a nonlinear impact angle control guidance law based on Lyapunov stability theory is proposed. The proposed law ensures the convergence of the heading angle and the miss distance to guarantee a successful engagement. The impact angle can be adjusted by varying a single parameter. And the maximum value of acceleration has been analyzed to get the proper range for control parameter. Considering the achievable impact angle set is limited, an additional phase is added to form a two-phase control strategy. The first phase is to establish a proper initial condition for the second phase, and the second phase is to hit the target with a certain impact angle. An analysis of the proper selection of control parameters to expand the achievable impact angle set is presented. The performance of the proposed guidance law is illustrated with simulations.  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号